[Wolfgang H]

Allerdings hab ich den A330-300.
Hier ist der Teil in dem ich Änderungen gemacht habe.
Der Reiseflug/Treibstoffverbrauch ist auf FL390 bei Mach:0.82 (260KIAS)optimiert.Falls Du die Verbräuche für den FS-Navigator gebrauchen kannst- sag Bescheid.

Sollte das rüberkopieren aus dem Forum nicht klappen- sag Bescheid.
Ansonst gilt auch das was mk116 geschrieben hat.
Gruss, Wolfgang

[General]
performance=Passengers\n2-class conf: 335 \n1-class conf: 440\n\nCargo\n32\/33 LD3 containers \/ 11 Pallets \n600 cubic Ft (17 cubic m)\nTotal lower hold volume: 5,656 cu ft \n\nDimensions\nSpan 197 ft 10 in\nLength 208 ft 11 in\nHeight 54 ft 11 in \n\nEngines: PW4000\nTO Thrust Rating: 68,000 lb\n\nMax Fuel Cap.: 24,700 gal\nMaxTOW: 467,400 lb\nZFW: 354,700 lb\n\nMax Range: 4,750 nm\nTypical Cruise Speed \n @ FL350: M.82
atc_type=AIRBUS
atc_model=A330

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000

max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000

empty_weight=354700.000

empty_weight_roll_MOI=8955743.000
empty_weight_pitch_MOI=22600873.000
empty_weight_yaw_MOI=22751035.000
empty_weight_coupled_MOI=1000.000

max_gross_weight=515700.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.853
induced_drag_scalar=0.703
elevator_effectiveness=1.205
aileron_effectiveness=1.500
rudder_effectiveness=2.502
pitch_stability=1.405
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000


[pitot_static]
vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI

[fuel]
Center1=0.000, 0.000, -4.000, 16260.000, 3.000
//Center2=-83.676, 0.000, 0.000, 1617.000, 3.000
LeftMain=-7.000, -37.983, 0.000, 3776.000, 3.000
LeftAux=-13.000, -70.269, 0.000, 974.000, 3.000
RightMain=-7.000, 37.983, 0.000, 3776.000, 3.000
RightAux=-13.000, 70.269, 0.000, 974.000, 3.000

fuel_type=2.000 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1

[airplane_geometry]
wing_area=3892.000
wing_span=197.833
wing_root_chord=20.000
wing_dihedral=6.218
wing_incidence=0.000
wing_twist=-0.500
oswald_efficiency_factor=0.600
wing_winglets_flag=1
wing_sweep=30.000
wing_pos_apex_lon=25.000
wing_pos_apex_vert=0.000
htail_area=1050.000
htail_span=69.700
htail_pos_lon=-89.200
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=40.000
vtail_area=690.000
vtail_span=27.300
vtail_sweep=35.000
vtail_pos_lon=-83.676
vtail_pos_vert=5.800
elevator_area=137.000
aileron_area=68.000
rudder_area=232.000
elevator_up_limit=24.000
elevator_down_limit=18.000
aileron_up_limit=25.000
aileron_down_limit=25.000
rudder_limit=45.000
elevator_trim_limit=15.000
spoiler_limit=35.000
spoilerons_available=0
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=9.969
min_flaps_for_spoilerons=0.000

[GeneralEngineData]
engine_type=1
Engine.0=15.166, -30.386, -7.583
Engine.1=15.166, 30.386, -7.583
fuel_flow_scalar=0.497

[TurbineEngineData]
bypass_ratio=5.00
fuel_flow_gain=0.001
inlet_area=54.522
rated_N2_rpm=29922.000
static_thrust=68000.000
afterburner_available=0
reverser_available=1

[jet_engine]
thrust_scalar=1.101

[Reference Speeds]
flaps_up_stall_speed=132.000
full_flaps_stall_speed=124.000
cruise_speed=460.000

[keyboard_response]
elevator=100.000, 200.000
aileron=100.000, 200.000
rudder=50.000, 100.000

[Views]
eyepoint=78.502, -1.756, 9.628

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=105.000
pitch_takeoff_ga=8.000
use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.

[direction_indicators]
direction_indicator.0=3,0